Gas turbine engine in-board cooled cooling air system
作者： Charles Lo
DOI:
关键词:
摘要: A system for supplying turbine cooling air flow includes a turbofan engine, heat exchanger, and door. The engine an case that has inner volume within which at least gas is mounted, bypass passage defined by outer fan duct configured to direct therethrough. exchanger disposed the coupled receive fluid from passage, transfer between air. door movably mounted in movable closed position, will not through open may exchanger.
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